SOLUTIONS OF THE GRUMMAN F-14 BENCHMARK CONTROL PROBLEM.
被引:7
作者:
Rimer, Melvyn
论文数: 0引用数: 0
h-index: 0
机构:
Grumman Aerospace Corp, Bethpage,, NY, USA, Grumman Aerospace Corp, Bethpage, NY, USAGrumman Aerospace Corp, Bethpage,, NY, USA, Grumman Aerospace Corp, Bethpage, NY, USA
Rimer, Melvyn
[1
]
Frederick, Dean K.
论文数: 0引用数: 0
h-index: 0
机构:
Grumman Aerospace Corp, Bethpage,, NY, USA, Grumman Aerospace Corp, Bethpage, NY, USAGrumman Aerospace Corp, Bethpage,, NY, USA, Grumman Aerospace Corp, Bethpage, NY, USA
Frederick, Dean K.
[1
]
机构:
[1] Grumman Aerospace Corp, Bethpage,, NY, USA, Grumman Aerospace Corp, Bethpage, NY, USA
来源:
IEEE Control Systems Magazine
|
1987年
/
7卷
/
04期
关键词:
COMPUTER SOFTWARE - Evaluation - CONTROL SYSTEMS - Computer Aided Design - MATHEMATICAL TECHNIQUES - Poles and Zeros;
D O I:
10.1109/MCS.1987.1105334
中图分类号:
学科分类号:
摘要:
In March 1985, an analysis benchmark problem was proposed for the evaluation of software for computer-aided control system design. The control system involved the longitudinal dynamics of the Grumman F-14 aircraft in level flight. Seven solutions have been received and evaluated, and the results are summarized here. Some observations are presented concerning the testing of software capabilities and the preparation of benchmark problems.